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Thanks from Bangladesh.
Mass flow rate is always conserved, even at the cross section of subsonic and supersonic flow at the throat
What is the size of the nozzle diameter relative to the size of the engine diameter?
Nicely explained . Keep it up
where can i see the equation derivation? i wonder how a simple adiabatic equation can turns out to be that complicated 😁👍
If you are young and readin this and get pimples....dont pop your pimples, they will scar, i wish someone told me when i was young
Thanks from Bangladesh.
Mass flow rate is always conserved, even at the cross section of subsonic and supersonic flow at the throat
What is the size of the nozzle diameter relative to the size of the engine diameter?
Nicely explained . Keep it up
where can i see the equation derivation? i wonder how a simple adiabatic equation can turns out to be that complicated 😁👍
If you are young and readin this and get pimples....dont pop your pimples, they will scar, i wish someone told me when i was young